System for measuring three-dimensional displacement

Abstract: A method for measuring three-dimensional displacement of a mass comprises the steps of providing a measuring object placed on the end surface of the mass, for reflecting at least a fraction of three-dimensional displacement of the mass, arranging a displacement measuring equipment for free displacement relative to the mass and in opposition to the measuring object, and measuring three-dimensional relative displacement of the mass by detecting relative displacement of sad displacement indicative means relative to the displacement measuring equipment by the latter. The method is implemented by a three-dimensional displacement measuring system comprises a measuring object placed on the end surface of the mass, for reflecting at least a fraction of three-dimensional displacement of the mass, a displacement measuring equipment arranged for free displacement relative to the mass and in opposition to the measuring object, for measuring three-dimensional relative displacement of the mass by detecting relative displacement of sad displacement indicative means relative to the displacement measuring equipment by the latter. The method and system is suitable for measuring displacement of a rock across a crack.

Description: The present invention relates generally to a system for measuring three-dimensional displacement of a mass. More specifically, the invention relates to a system suitable for measuring three-dimensional displacement of a discontinuous surface, such as a crack in a rock or a natural joint and so forth. Conventionally, in fields of mechanical engineering, civil engineering and so forth, a non-contact type distance measuring equipment, such as a laser type displacement gauge, or a contact type displacement gauge employing a differential transformer and so forth are used practically. Namely, these measuring equipments performed high precision measurement of a displacement of a mass as an object for measurement (hereinafter referred to as measuring object) as a relative displacement from a reference portion where various displacement gauges are placed. Also, particularly in the field of civil engineering and mining, or in the field of geophysics, measurement of displacement of a foundation, such as a rock, is performed for appropriately evaluating behavior of rock or crust. As a method for measuring the displacement of the foundation, a measuring method employing an extensometer is typically employed. Namely, this method makes analysis of the displacement of the foundation by setting a fixed measuring point within a bore hole formed in the foundation, such as the rock, and measuring a variation of a distance between the fixed measuring point and a measuring point located at the opening end of the bore hole on the earth by means of the extensometer. However, when the displacement of the mass is measured by the conventional measuring system and method, the relative displacement from the reference portion where the displacement gauge is located is merely measured as a linear relative displacement. Therefore, in order to measure the three dimensional displacement of the mass, displacement measurements by means a plurality of measuring equipments which are arranged three-dimensionally. This makes installation of the measuring equipments and collection of measured data complicate. Furthermore, in particular, when three-dimensional behavior of the foundation is to be evaluated by the extensometer, since the measuring method employing the extensometer permits only evaluation of relative linear displacement between two measuring points along an axis of the bore hole, it is inherent to three-dimensionally arrange a plurality of bore holes to perform multi-axes and multi-point measurement for three-dimensional evaluation. In addition, in the method, it is not possible to instantly detect behavior discontinuous surface, such as crack of the rock, natural joint or so forth which sensitively reflects variation of stress condition of the foundation. Namely, in the conventional method employing the extensometer, a problem is encountered in requiring a huge amount of experiments for performing multi-axes and multi-points measurement for evaluating the three-dimensional behavior of the foundation. Also, the conventional method cannot make analysis of the behavior by specifying the discontinuous surface but rather unitarily evaluates deformation of the discontinuous surface associating with variation of the stress condition in the foundation and displacement of the foundation as a continuous body. Therefore, it is not possible to perform evaluation by specifying deformation of the discontinuous surface primarily determining deformation of the foundation. In the prior art, a further problem is encountered in impossibility of proper evaluation of relationship between the behavior of the overall foundation and the behavior of the discontinuous surface, deformation direction, deformation magnitude. EP-A-0 493 651 discloses a system for the detection of the position and orientation of an object in space, in particular a helmet. The helmet has passive reflectors for reflecting a scanning light beam from a laser source. The return times and directions of the returning light beam relative to a return of a light beam from a reference point, processed by the off-helmet electronics, result in a position indication of the helmet. WO-A-84/02771 discloses a device for determining a modification of the relative distance between two measurement points, in particular in cavities structures, where the walls often need a long time to stabilize. In order to determine whether rock displacements may occur and to which extent they may occur, measurement instruments are incorporated into the walls at opposite locations. A cardan suspended pendulum has a light source at its bearing point and a light receiver at its pendulum mass. On the opposite wall a mirror is arranged with an inclination with respect to the vertical. A displacement of the mirror provides an indication to the light receiver. The present invention has been worked out in view of the problems set forth above, and, therefore, it is an object of the present invention to provide a system for measuring three-dimensional displacement which does not require displacement measurement with three-dimensionally arranged plurality of measuring equipments and can easily measure three-dimensional displacement of a mass. Another object of the present invention is to provide a three-dimensional displacement measuring system which can easily evaluate three-dimensional behaviour of foundation without requiring multi-axes and multi-point measurement and permits high precision and effective evaluation of deformation of the foundation by specifically measuring deformation of a discontinuous surface primarily determining most of deformation of the foundation. According to the invention, there is provided a three-dimensional displacement measuring system comprising: a concave surface formed of a curved surface converging from the opening end to the bottom placed on the end surface of a mass, for reflecting at least a fraction of three-dimensional displacement of said mass; a displacement measuring means arranged for free displacement relative to said mass and in opposition to said concave surface, said displacement measuring means measuring relative distance to said concave surface along a circumferential trace by rotating about a centre axis of said concave surface while maintaining a given tilt angle relative to said centre axis for circumferentially scanning said concave surface. The system may further comprise means for making analysis of the displacement of the circumferential trace on the concave surface associating with the displacement of the mass, on the basis of the relative distance measured by the displacement measuring equipment. The displacement measuring equipment may comprise a non-contact type measuring equipment which does not contact with the concave surface. The non-contact type measuring equipment may be a laser displacement gauge irradiating a laser beam in oblique to the centre axis of the concave surface, for example. The displacement measuring equipment may include a rotary table having a rotary shaft arranged in alignment with the centre axis of the concave surface and driven by a motor, and the laser displacement gauge is mounted on the rotary table. The mass may comprise a first cylindrical member arranged at one side of a discontinuous surface in a bore hole formed across the discontinuous surface. The first and second cylindrical members may have fixing means press fitted onto the peripheral wall surface of the bore hole for fixing the first and second cylindrical members within the bore hole. The fixing means may comprise a fixing rod slidably extending radially through each of the cylindrical members. Other objects, features and advantages of the present invention will become clear from the detailed description given hereinafter with reference to the accompanying drawings. The present invention will be understood more fully from the detailed description given herebelow and from the accompanying drawings of the preferred embodiment of the present invention, which, however, should not be taken to be limitative to the invention, but are for explanation and understanding only. In the drawings: Fig. 1 is an explanatory illustration showing a manner for measuring a three-dimensional displacement of a mass by means of one embodiment of a three-dimensional displacement measuring system according to the present invention; Fig. 2 is an illustration showing an example of a curved plane forming a concave surface; Figs. 3(A) to 3(D) are illustrations for explaining a principle of measurement of three-dimensional displacement of the mass by the present invention; Fig. 4 is a fragmentary illustration showing another embodiment of the three-dimensional displacement measuring system according to the present invention, adapted for measurement of displacement of a discontinuous surface of a rock; Fig. 5 is a section showing a further embodiment of the three-dimensional displacement measuring system according to the present invention, adapted for measurement of displacement of a discontinuous surface of a rock; Fig. 6 is an enlarged view of a part of the three-dimensional displacement measuring system of Fig. 5 ; and Fig. 7 is a section showing one example of a differential transformer displacement gauge in the three-dimensional displacement measuring system OF Fig. 5 . The preferred embodiments of a three-dimensional displacement measuring system and method will be discussed hereinafter in detail with reference to the accompanying drawings. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. It will be obvious, however, to those skilled in the art that the present invention may be practiced without these specific details. In other instance, well-known structures are not shown in detail in order to unnecessary obscure the present invention. Fig. 1 shows a manner of measurement of a three-dimensional displacement of a rigid block 11 as a measuring object, employing the first embodiment of a three-dimensional displacement measuring system 10 according to the present invention. The three-dimensional displacement measuring system 10 comprises a concave surface 12 formed on the rigid block 11 , and a displacement measuring equipment 13 provided above the opening portion of the concave surface 12 and supported by a stationary base 14 in opposition to the concave surface 12 . The concave surface 12 converges toward a bottom thereof from the opening portion and is formed of a curved surface expressed by a mathematical equation. For example, as shown in Fig. 2 , the concave surface defines a configuration of a conical, truncated conical, hyperboloid, conicoid, hemisphere, pyramid, triangular pyramid or so forth. Also, the concave surface 12 is processed by surface finishing to provide a smooth surface so that a distance measurement by means of a laser displacement gauge 19 which will be discussed later, can be performed accurately. On the other hand, the displacement measuring equipment 13 comprises an upper rotary disc 15 and a lower rotary disc 16 arranged at both sides of the stationary base 14 , a rotary table 17 rotatable about a rotary shaft 18 positioned in alignment with a center axis X of the concave surface 12 , and the laser displacement gauge 19 mounted on the lower rotary disc 16 . The rotary table 17 is driven by a rotation control motor 20 via the upper rotary disc 15 engaging with the motor. The laser displacement gauge 19 is mounted in an orientation directed to a direction Y which is oblique to the center axis X of the concave surface 12 . By this arrangement, a laser beam irradiated from the laser displacement gauge 19 impinges on the curved surface forming the concave surface 12 and then reflected to return to the laser displacement gauge 19 . By this, a relative distance between the laser displacement gauge and a reflection point. It should be noted that such type of the laser displacement gauge is per se known in the art. According to rotation of the rotary table 17 , the center axis of the laser displacement gauge 19 , namely the irradiation axis Y of the laser beam is shifted circumferential direction with defining a conical trace. On the other hand, the reflection point of the laser beam defines a circular trace on the concave surface 12 by rotatingly scanning the laser beam on the concave surface. The rotary shaft 18 of the rotary table 17 extends through a through hole 21 defined in the stationary base 14 . A ball bearing 22 is disposed within the through hole 21 for permitting smooth rotation of the rotary table 17 . With the shown embodiment of the three-dimensional three-dimensional displacement measuring system 10 , displacement, including back and forth displacement, left and right displacement, rotational displacement of the rigid block 11 . Namely, when displacement is caused in the rigid block 11 , a trace of an intersection between the circumferentially shifting laser beam with defining a conical trace and the concave surface 12 having a surface configuration, such as conical configuration surface, hyperboloid configuration surface and so forth, i.e. the trace of the reflection point of the laser beam, shifts three-dimensionally. The displacement of the trace of the laser beam reflection point on the concave surface 12 is analyzed according to the following principle for easily measuring the displacement of the rigid block 11 as a relative displacement from the displacement measuring equipment 13 . The principle of deriving the displacement of the rigid body 11 is as follow. Here, for the purpose of disclosure, rotational displacement of the rigid block will be ignored for simplification of the disclosure. However, it is, of course, possible to perform with taking the rotational displacement of the rigid body into account. 1) Assuming the trace defined by the irradiation axis Y of the laser beam is expressed by an equation for conical configuration as follow: f(x, y, z) = 0 ( Fig.3(A) ) 2) The equation of the concave surface 12 arranged in opposition to the laser displacement gauge is expressed by: g(u, v, w) = 0 ( Fig.3(B) ) 3) z axis is parallel to w axis. Under the condition set forth above, a relationship of both coordinate axes can be expressed by: x = u + a y = v + b z = w + c (where, a, b, c are offset in x direction, y direction and z direction of the coordinate center of (u, v, w).) 4) By this, the equation of the curve (this expresses the rotational trace of the reflection point) when two curved surfaces intersect as follow: f(x, y, z) = g(x-a, y-b, z-c) Here, for the purpose of disclosure, it is assumed that (x, y, z, a, b, c) = 0 5) Assuming that the length measured by the displacement gauge is r and the angle is , the relationship between the distance r, angle  and (x, y, z) can be expressed as follows: x = r • cos α • cos  y = r • cos α • sin  z = -r • sin α 6) Accordingly, the trace defined on the concave surface 12 by the measured value (r and ) can be expressed by: h(r • cos α • cos , r • cos α • sin , -r • sin α) = 0 Therefore, it can be expressed by; t(r, , a, b, c) = 0 7) From the measured trace, a, b, c satisfying the foregoing function may be derived by way of optimization method, such as a method of least squares or so forth. 8) Since a, b, c can be derived in each measurement, the three dimensional displacement can be easily calculated by comparing a, b, c derived at respective measurements. Fig. 4 shows another embodiment of the three-dimensional displacement measuring system 30 according to the present invention. The shown embodiment of the three-dimensional displacement measuring system 30 is intended to be employed in evaluation of behavior of foundation. The three-dimensional displacement measuring system 30 is disposed within a bore hole 33 formed across a discontinuous surface, such as a crack 32 of the rock or so forth. The three-dimensional displacement measuring system 30 includes a first cylindrical member 34 as a mass located in one side of the rock 31a and a second cylindrical member 35 located in the other rock 31b opposing to the rock 31a across the crack 32 and following to the first cylindrical member 34 . The first cylindrical member 34 defines a concave surface 40 formed with a predetermined curved surface, such as conical, truncated conical, hyperboloid, conicoid, hemisphere, pyramid, triangular pyramid, converging from the opening end to the bottom, at the rear end thereof. In the vicinity of the center of the first cylindrical member 34 , a radially extending fixing rod 36 is provided. The fixing rod 36 has an expanding and contracting device (not shown) constructed with a combination of a hydraulic cylinder and a spring. The expanding and contracting device is connected to a pressure line 37 to receive a hydraulic pressure controllably supplied from a working base at the opening end of the bore hole 33 on the earth. The expanding and contracting device is responsive to the hydraulic pressure supplied through the pressure line 37 to drive a fixing pin 38 and a hole wall abutment 39 provided at both axial ends of the fixing rod 36 to cooperatively extend from or contract into the fixing rod. Namely, in the action, when the fixing pin 38 is driven toward left to protruded, the hole wall abutment 39 is driven to be retracted. On the other hand, at the tip end of the second cylindrical member 35 , a displacement measuring equipment 41 is mounted in opposition to the concave surface 40 formed at the read end of the first cylindrical member 34 . The displacement measuring equipment 41 comprises a rotary table 44 rotatably supported on a support frame 49 mounted on the tip end surface of the second cylindrical member 35 , and a laser displacement gauge 50 fixed on the rotary table. The rotary table 44 has a front rotary disc 42 and a rear rotary disc 43 mutually coupled through a rotary shaft 45 extending in alignment with the center axis X of the concave surface 40 . The rotary table 44 is rotatingly driven by a rotation control motor 46 engaging with the rear rotary disc 43 . The laser displacement gauge 50 is mounted on the front rotary disc 42 and oriented to direct the laser beam axis Y in oblique to the center axis X of the concave surface 40 . The laser beam irradiated from the laser displacement gauge 50 impinge onto the curved surface forming the concave surface to be reflected thereon. The laser beam axis Y is shifted according to rotation of the rotary table 44 with defining substantially conical trace. Therefore, according to circumferential scanning of the laser beam on the concave surface 40 , the reflecting point is shifted to form a circular trace. On the other hand, in the vicinity of the axial center position, the fixing rod 36 having the identical construction to that provided in the first cylindrical rod 34 is provided. Within a gap between the first cylindrical member 34 and the second cylindrical member 35 , a membrane wall 47 as a water-tight seal member, is mounted surrounding the concave surface 40 and the displacement measuring equipment 41 for protecting the latter. Also, on the external surfaces of the first and second cylindrical members 34 and 35 , a plurality of supporting legs 51 are arranged with a given interval in the circumferential direction at both circumferential sides of the fixing pins 38 of the fixing rods 36 . These supporting legs 51 are cooperative with the hole wall abutments 39 of the fixing rod 36 when the hole wall abutments 39 are projected from the fixing rod to abut against the hole wall, so as to fix the first and second cylindrical members 34 and 35 at respectively predetermined positions within the bore hole 33 . For making analysis of behavior of the crack 32 in the rock by the three-dimensional displacement measuring system 30 , the three-dimensional displacement measuring system 30 is initially set in respectively predetermined positions in the rocks 31a and 31b opposing across the crack 32 . Upon installation, the first and second cylindrical members 34 and 35 are integrally secured on a carriage having sliding mechanism, such as wheels or casters. The first and second cylindrical members 34 and 35 are secured on the carriage by projecting the fixing pins 38 of the fixing rods 36 and engaging the fixing pins to the carriage. When the first and second cylindrical members 34 and 35 with the carriages are pushed into the bore hole 33 to place at respectively predetermined positions. Thereafter, the hydraulic pressure is supplied to the expanding and contracting devices in the fixing rods 36 via the pressure lines 37 to force the hole wall abutments 39 to firmly abut on the peripheral wall of the bore hole 33 to fix the first and second cylindrical members 34 and 35 at respectively predetermined positions. It is preferred to mount a bore hole television camera or so forth on the carriage so as to facilitate retrieval of the crack 32 . Furthermore, by mounting the bore hole television camera or so forth, respective of the first and second cylindrical members 34 and 35 may be accurately fixed at the predetermined positions. At the same time of fixing the three-dimensional displacement measuring system 30 within the bore hole 33 , the fixing pins 38 are driven to be retracted to release the first and second cylindrical members 34 and 35 from the carriage. Therefore, the carriage can be easily removed from the bore hole 33 . It should be noted that installation of the measuring equipment at the predetermined positions will be described in more concrete manner in another embodiment discussed later. After installation of the three-dimensional displacement measuring system 30 at the predetermined positions, the relative displacement between the first cylindrical member 34 positioned within one of the rock 31a and the second cylindrical member 35 positioned within the other rock 31b is measured for making analysis of the specified crack 32 . Namely, when the rocks opposing across the crack is relatively displaced, the first and second cylindrical members 34 and 35 are similarly displaced relative to each other. Therefore, similarly to the embodiment of Fig. 1 , the trace of the intersection between the laser beam axis Y shifted to define a conical trace and the concave surface 40 , namely the circular trace of the reflection point is displaced three-dimensionally. It should be appreciated that the three-dimensional displacement measuring system 30 is connected to a CPU (not shown) for performing measurement control, arithmetic operations, data file management and so forth, a data recording memory (not shown) and so forth via various connection lines so that analysis of the behavior of the crack 32 can be performed instantly. With the three-dimensional displacement measuring system 30 constructed as set forth above, by specifying the crack 32 which primarily determines most of deformation of the foundation as the discontinuous surface, the behavior of the crack can be easily analyzed with high precision to facilitate evaluation of the three-dimensional behavior of the foundation. It should be noted that while the foregoing embodiments are discussed in terms of use of the known laser type displacement gauge as the displacement gauge, it is possible to employ other of non-contact type distance measuring equipments or contact-type displacement gauge, such as that employing the differential transformer. When the contact type displacement gauge is used, it is desirable to provide a rotary ball or so forth at the tip end of the displacement gauge so that the displacement gauge may smoothly move on the concave surface 12 or 40 in circumferential direction. A further embodiment of the three-dimensional displacement measuring system according to the invention will be discussed with reference to Figs. 5 to 7 . The three-dimensional displacement measuring system 60 illustrated in these figures is designed for measuring displacement of the crack in the rock as one example of the discontinuous surface. The three-dimensional displacement measuring system 60 generally comprises a measuring object 61 disposed in the bore hole 33 formed in the rock across the crack 32 and located in the rock 31a positioned at one side of the crack 32 , a displacement measuring equipment 62 located within the rock 31b at the other side of the crack and following to the measuring object 61 , and a fixing guide member 63 detachably attached to the measuring object 61 and the displacement measuring equipment 62 . As shown in enlarged section of Fig. 6 , the measuring object 61 has a first cylindrical portion 64 having a tip end with a smaller diameter. On the read end surface of the first cylindrical member 64 , a surface member 65a is mounted with orienting the surface in parallel to the rear end surface of the first cylindrical member. Another pair of surface members 65b (only one is shown) are oriented perpendicularly to the surface member 65a and extending rearwardly. The pair of surface members 65b also intersects perpendicularly to each other. The first cylindrical memnber 64 carries a fixing rod 66 . The fixing rod 66 has an expanding and contracting device constructed with a combination of a hydraulic cylinder and a spring. The expanding and contracting device is connected to a pressure line 67 to receive a hydraulic pressure controllably supplied from a working base at the opening end of the bore hole 63 on the earth. The expanding and contracting device is responsive to the hydraulic pressure supplied through the pressure line 67 to drive a fixing pin 68 and a hole wall abutment 69 provided at both axial ends of the fixing rod 66 to cooperatively extend from or contract into the fixing rod. Namely, in the action, when the fixing pin 68 is driven toward left to protruded by application of the hydraulic pressure, the hole wall abutment 69 is driven to be retracted. On the other hand, by releasing the hydraulic pressure, the fixing pin 68 is retracted and the hole wall abutment 69 is projected. On the other hand, the displacement measuring equipment 62 has a second cylindrical member 70 following the first cylindrical member 64 . On the tip end surface (the surface opposing to the read end surface of the first cylindrical member 64 where the three surfaces 65 , i.e. surface members 65a and 65b , a support base 71 is rigidly secured. On the support base 71 , three differential transformer displacement sensor (hereinafter referred to as "LVDT displacement sensor) 72 are mounted. Each LVDT displacement sensor 72 is arranged to perpendicularly mate with corresponding one of the three surfaces of the surface members 65a and 65b . The second cylindrical member 70 also includes the fixing rod 66 having the identical construction to that provided in the first cylindrical member 64 . At a gap between the first and second cylindrical members 64 and 70 , a membrane wall 74 serving as a water-tight seal is mounted with covering the three surface members 65 and the LVDT displacement sensor 72 for protruding the latter. On the external surface of the first and second cylindrical members 64 and 70 , a plurality of supporting legs 74 are arranged with a given interval in the circumferential direction at both circumferential sides of the fixing pins 68 of the fixing rods 66 . These supporting legs 74 are cooperative with the hole wall abutments 69 of the fixing rod 66 when the hole wall abutments 69 are projected from the fixing rod to abut against the hole wall, so as to fix the first and second cylindrical members 64 and 70 at respectively predetermined positions within the bore hole 33 . The LVDT displacement sensor 72 is per se known in the art. For example, the LVDT displacement sensor 72 comprises a primary coil 76 , a secondary coil 77 , a differential transformer portion 75 including a core 78 formed of a magnetic body and disposed at the center of the primary and secondary coils, a measuring element 79 , a spindle 80 , a measuring pressure spring 81 and so forth. The measuring element 79 is held in contact with the surface members 65a and 65b of the three surfaces 65 and adapted to be shifted in axial direction according to displacement of the corresponding surface member. The magnitude of shifting of the measuring element 79 is detected by exciting the primary side of the differential transformer portion 75 by an alternating current, generating a secondary signal proportional to the shifting magnitude of the measuring element 79 which is directly connected to the core 78 via the spindle 80 , detecting the secondary signal to output as a direct current signal indicative of the shifting magnitude of the measuring element 79 , and in turn indicative of the displacement of the three surfaces 65 . The fixing guide member 63 comprises a thin plate member 82 curved along the external surfaces of the first and second cylindrical members 64 and 70 . The circumferential width of the plate member 82 is determined so that it may be placed between the support legs 74 . For the plate member 82 , engaging holes 83 for engaging with the fixing pins 68 of the d ixing rods 66 are formed. Therefore, by projecting the fixing pins 68 to engage with the engaging holes 83 , the measuring object 61 including the first cylindrical member 64 and the displacement measuring equipment 62 including the second cylindrical member 70 are fixed on the fixing guide member 63 . At this condition, the measuring object 61 and the displacement measuring equipment 62 are fixedly connected to each other and thus prevented from relative displacement. The support leg 74 maintains a clearance between the peripheral wall surface of the bore hole 33 and the external peripheries of the cylindrical members 64 and 70 for protecting the fixing guide member 83 and facilitate withdrawal of the fixing guide member 63 . As shown in Fig. 5 , as a supporting carriage is provided in the fixing guide member 63 , a wheeled centrizer 84 is provided. The plate member 82 set forth above is extended frontwardly from the wheeled centrizer 84 . To the wheeled centrizer 84 , an extension rod 85 reaching the opening end of the bore hole is connected. Also, the wheeled centerizer 84 carries a bore hole television camera 86 for visually monitoring the wall surface of the bore hole 33 . It should be noted that the LVDT sensor 72 of the displacement measuring equipment 62 is connected to an amplifier of the LVDT displacement sensor, an A/D converter, a CPU for performing measuring control and data file management, a data memory and so forth via various connection lines. For measuring the displacement of the crack 32 in the rock employing the three-dimensional displacement measuring system 60 as set forth above, the three-dimensional displacement measuring system 60 is disposed within the bore hole 33 across the crack 32 . The installation of the three-dimensional displacement measuring system is performed through the following process. The measuring object 61 and the displacement measuring equipment 62 are inserted into the bore hole 33 in a condition fixed to each other by the fixing guide member 63 . By connecting extension rods 85 , the assembly of the measuring object 61 and the displacement measuring equipment 62 are pushed to the predetermined positions in the bore hole 33 with sliding of the fixing guide member 63 . Since the fixing guide member 63 includes the wheeled centrizer 84 , the assembly of the measuring object 61 and the displacement measuring equipment 62 with the fixing guide member 63 can be smoothly moved within the bore hole 33 . During movement of the assembly of the measuring object 61 and the displacement measuring equipment 62 , the bore hole television camera 86 picks up the image of the peripheral wall of the bore hole 33 for visual display, the accurate position of the crack 32 can be detected. One the accurate position of the crack 32 is detected by means of the bore hole television camera 86 , the fixing guide member 63 is pulled back for a predetermined stroke. Then, the positions of the measuring object 61 within the rock 31a at one side of the crack 32 and the displacement measuring equipment 62 within the rock 31b at the other side of the crack 32 are adjusted to place them at respectively predetermined positions. Thereafter, the hydraulic pressure applied to the expanding and contracting device of the fixing rod 66 is drained so that the spring therein overcomes the hydraulic force to retract the fixing pins 68 away from the engaging holes 83 , and at the same time, to protrude the hole wall abutment 69 to establish pressure contact thereon. Accordingly, the engagement between the fixing pins 68 and the engaging holes 83 is released to place the measuring object 61 and the displacement measuring equipment 62 free from fixing guide member 63 . Simultaneously, abutment of the hole wall abutment onto the peripheral wall surface of the bore hole 33 in cooperation with the supporting legs 74 causes the measuring object 61 and the displacement measuring equipment 62 rigidly fixed at respectively predetermined positions in the bore hole 33 . By this installation of the three-dimensional displacement measuring system 60 is completed. Attention should be attracted to the fact that the measuring object 61 and the displacement measuring equipment 62 are held in the fixed position on the fixing guide member 63 until the three-dimensional displacement measuring system 60 is set in the bore hole 33 . In this manner, the relative position between the measuring object 61 and the displacement measuring equipment 62 are maintained at fixed condition. By this, narrowing of the measuring range, offsetting out of measuring range and error in measurement of the LVDT displacement sensor 72 due to offset of the initial fixing position can be successfully avoided, The fixing guide member 63 which is released from the measuring object 61 and the displacement measuring equipment 62 as fixing of the latter in the bore hole 33 is removed together with the bore hole television camera 86 via the extension rod 85 . When the rock 31a displaces relative to the rock 31b mating across the crack 32 , the measuring object 61 also displaces relative to the displacement measuring equipment 62 . This relative displacement appears as displacement of any one or more of the three surfaces 65 of the surface members 65a and 65b to cause shifting of the corresponding measuring element or elements 79 . Thus, by monitoring displacement of the three surfaces 65 by three LVDT displacement sensors 72 , the relative displacement of the foundation positioned across the crack 32 can be monitored with high precision. As set forth above, the LVDT displacement sensors 72 of the displacement measuring equipment 62 are connected to the amplifiers of the LVDT displacement sensors 72 , the A/D converter, the CPU performing measurement control and data file management, the data recording memory and so forth. Therefore, the behavior of the crack can be monitored automatically for a long period. It should be noted that when a predetermined period is elapsed and measurement is completed, the hole wall abutments 69 are released from engagement with the peripheral wall of the bore hole. Then, the three-dimensional displacement measuring system 60 can be recovered from the bore hole via the pressure line 67 . Here, when step is formed in the bore hole 33 due to deformation of the rocks, the displacement measuring equipment 62 may be separated from the measuring object 61 so that it may solely recovered. It should be noted that although the shown embodiment employs three mutually perpendicularly intersecting surfaces for monitoring three-dimensional behavior of the crack 32 , it is naturally possible to employ more surfaces for measuring displacement. Although the invention has been illustrated and described with respect to exemplary embodiment thereof, it should be understood by those skilled in the art that the foregoing and various other changes, omissions and additions may be made therein and thereto, without departing from the scope of the present invention. Therefore, the present invention should not be understood as limited to the specific embodiment set out above but to include all possible embodiments which can be embodied within the scope encompassed by the appended claims.

Claims: A three-dimensional displacement measuring system comprising: a concave surface (12,40) formed of a curved surface converging from the opening end to the bottom and having a centre axis (X), said concave surface being placed on the end surface of a mass, for reflecting at least a fraction of three-dimensional displacement of said mass; a displacement measuring means (13,45) arranged for free displacement relative to said mass and in opposition to said concave surface, said displacement measuring means measuring relative distance to said concave surface (12,40) along a circumferential trace by rotating about a centre axis (X) of said concave surface while maintaining a given tilt angle relative to said centre axis for circumferentially scanning said concave surface (12,40). A system as set forth in claim 1, which further comprises means for making analysis of the displacement of said circumferential trace on said concave surface associated with the displacement of said mass, on the basis of said relative distance measured by said displacement measuring means (13,45). A system as set forth in claim 1, wherein said displacement measuring means comprises a non-contact type measuring equipment which does not contact said concave surface (12). A system as set forth in claim 3, wherein said non-contact type measuring means is a laser displacement gauge (19) irradiating a laser beam obliquely to the centre axis (X) of said concave surface (12). A system as set forth in any preceding claim, wherein said displacement measuring means includes a rotary table (17,44) having a rotary shaft (18,45) arranged in alignment with the centre axis (X) of said concave surface (12,40) and driven by a motor (20,46). A system as set forth in any preceding claim, wherein said mass comprises a first cylindrical member (34) arranged at one side of a discontinuous surface in a bore hole, formed across said discontinuous surface, and said displacement measuring means comprises a second cylindrical member (35) positioned at the other side of said discontinuous surface. A system as set forth in claim 6, wherein said bore hole is formed in a rock and said discontinuous surface is a crack in the rock. A system as set forth in claim 6, wherein respective of said first and second cylindrical members are provided with supporting legs and fixing rods adapted to be press fitted to the inner periphery of said bore hole.

Inventors: KOSUGI MASAYUKI, TAMAI AKIO, KOSUGI, MASAYUKI, TAMAI, AKIO
Applicants: AGENCY IND SCIENCE TECHN, OHBAYASHI CORP, AGENCY OF INDUSTRIAL SCIENCE AND TECHNOLOGY, OBAYASHI CORPORATION
Application year: 1994
Main classification: E21B47
IPC codes: E21B49, H01L27, E21B47, G01B5, E21F17, G01B11, G01B7